conceptual design and analysis of long span structure
TRANSCRIPT
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CONCEPTUAL DESIGN AND ANALYSIS OF LONG SPAN STRUCTURES
Massimo Majowiecki – IUAV University of Venice, Italy
Key words: structural architecture, wide span structures , reliability, experimental analysis,
monitoring.
ABSTRACT
Long span roof are today widely applied for sport, social, industrial, ecological and other
activities. The experience collected in last decades identified structural typologies as space
structures, cable structures, membrane structures and new - under tension - efficient materials
which combination deals with lightweight structural systems, as the state of art on long span
structural design. In order to increase the reliability assessment of wide span structural
systems a knowledge based synthetic conceptual design approach is recommended.
Theoretical and experimental in scale analysis, combined with a monitoring control of thesubsequent performance of the structural system, can calibrate mathematical modelling and
evaluate long term sufficiency of design.
INTRODUCTION
Long span structures are today widely applied mainly for sport buildings as:
− Stadia− Sport halls− Olympic swimming pools− Ice tracks and skating rinks− Indoor athletics
The state of the art trend on widespan enclosures: the lightweight structures - from
compression to tension.
According to the state of the art, the more frequently typologies and materials used for wide
span enclosures are:
Space structures
− single layer grids− double and multi layer grids− single and double curvature space
frames [1]
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Cable structures
− cable stayed roofs− suspended roofs− cable trusses
− singleand multilayer nets
Membrane structures
− prestressed anticlastic membranes− pneumatic membranes
Hybrid structures
− tensegrity systems− beam-cable systems
Convertible roofs
− overlapping sliding system− pivoted system− folding system [3]
The historical trend in the design and construction process of wide span enclosures was and is
the minimization of the dead weight of the structure and , consequently, the ratio between
dead and live loads (DL/LL).
From ancient massive structures (DL/LL>>1) to modern lightweight structures (DL/LL
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In Table 1, is possible to observe the exceptionally efficiency of steel and hi-tech materials
observing the strength to weight ratio (K=σ / γ ) in tension (Kt).The different mechanical behaviour of compression and tension structures can be illustrated
by Fig.1 where, starting from a thin parabolic arch under uniform distributed load , it is
possible to observe, during incremental loading, the following phases of the load
displacement curve:− Phase A: unloaded structure.− Phase AB: compression phase; geometric softening; decrease of tangential stiffness,reduction in the positive value of the secondary term of the total potential energy π δ 2 .
− Phase BCE: unstable phase; dynamic displacement from B to E with liberation of kineticenergy (cross hatched area). Here, the secondary term of total potential energy is negative
( 02 π δ ). Phase DEF is characteristic of the behaviour of tension structures. The non-linear
geometric hardening results in a less than proportional increase of stresses in relation to
increase external loads. This provides an increased nominal safety factor evaluated at ultimate
limit state (β safety index).
MATERIALSσt
R
N/m
m²
σcR
N/m
m²
γ k N/m
3
103
Ktm
Kc m
Bricks 3 18 166
Wood 85 37.5 5 21.2509.37
5
Concrete 30 251.20
0
S 355 520 79.5 6.664 ----
S 460 640 79.5 8.050
S 690 860 79.5 10.080
Steel 105 1050 79.5 13.376 ----
Titanium 900 45 20.000 ----
Composite materials hi-tech
Fig.1 Mechanical behaviour from arch to cableUnidir. Carbon
fibres
1400 15.5 90.000
Textile carbon
fibres
800 15.5 52.000 ----
Unidir.Aramidicfibres
1600 13 123.000 ----
Textile aramidicfibres (Kevlar)
750 13 58.000 ----
Unidir. Glassfibres
1100 20 55.000 ----
Textile glass
fibres
450 20 22.500 ----
TECHNOLOGY
ART
EXPERIENCE
NATURE SYNTHESISDESIGN
IDEA
E S T H E T I C S
I N T U I T I O N
E T H I C S
I N F O R M A T I C S
K N O W L E D G E
C O D E S
OBSERV.
SCIENCE
RESEARCH
Table 1. Mechanical properties of constructionmaterials
Fig.2 Holistic approach to structural design
CompressionStructures
DL/LL ↑ σ/γ ↓ β ↓
Tension Structures
DL/LL ↓ σ/γ ↑ β ↑
Static instability
δ²π0δ²π
Hardeninginconditionally stable
π>0δ²π
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1. KNOWLEDGE BASED CONCEPTUAL DESIGN AND RELIABILITY LEVEL
The conceptual design is knowledge based and, basically, property of individual experts.
Their involvement in early stages of design is equivalent, from the reliability point of view, to
a human intervention strategy of checking and inspection and, from a statistical point of view,
to a "filtering" action which can remove a significant part of “human errors”.According to the design requirements, the conceptual design is defined by a knowledged
expert synthetical approach based on the reliability intuition of the selected model which has
to be confirmed by the results of the analysis phase. The conceptual design approach is
holistic and directly depends on the skills and abilities of the design team members (Fig. 2).
1.1. Special aspects of conceptual design decisions on long span structures.
Considering the “scale effect” of long span structures several special design aspects arise as
[2]:
− the snow distribution and accumulations on large covering areas in function of statisticallycorrelated wind direction and intensity;
− the wind pressure distribution on large areas considering theoretical and experimentalcorrelated power spectral densities or time histories;
− rigid and aeroelastic response of large structures under the action of cross-correlated randomwind action considering static, quasi-static and resonant contributions;
− the time dependent effect of coactive indirect actions as pre-stressing, short and long termcreeping and temperature effects;
− the local and global structural instability;− the non linear geometric and material behaviour;
− reliability and safety factors of new hi-tech composite materials;− the necessity to avoid and short-circuit progressive collapse of the structural system due tolocal secondary structural element and detail accidental failure;
− the compatibility of internal and external restrains and detail design, with the modellinghypothesis and real structural system response;
− the parametric sensibility of the structural system depending on the type and degree of staticindeterminacy and hybrid collaboration between hardening and softening behaviour of
substructures.
− In the case of movable structures, the knowledge base concerns mainly the moving cranesand the related conceptual design process have to consider existing observations, tests and
specifications regarding the behaviour of similar structural systems. In order to fill the gap,the IASS working group n°16 prepared a state of the art report on retractable roof structures
including recommendations for structural design based on observations of malfunction and
failures [3].
From the observations of the in service performance, damages and collapses of all or part of
structural systems, we have received many informations and teachings regarding the design
and verification under the action of ultimate and serviceability limit states.
Long span coverings were subjected to partial and global failures as that of the Hartford
Colisseum (1978), the Pontiac Stadium (1982) and the Milan Sport Hall (1985) due to snow
storms, the Montreal Olympic Stadium due to wind excitations of the membrane roof (1988)
and snow accumulation (1995), the Minnesota Metrodome (1983) air supported structure that
deflated under water ponding, the steel and glass shell sporthall in Halstenbeck (2002), the
acquapark in Moscow and the air terminal in Paris (2004). Those cases are lessons to be
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learned from the structural failure mechanism in order to identify the design and construction
uncertainties in reliability assessment. Many novel projects of long span structures attempt to
extend the "state of the art". New forms of construction and design techniques generate
phenomenological uncertainties about any aspect of the possible behaviour of the structure
under construction service and extreme conditions.
Fortunately, structures rarely fail in a serious manner, but when they do it is often due tocauses not directly related to the predicted nominal loading or strength probability
distributions. Other factors as human error, negligence, poor workmanship or neglected
loadings are most often involved. Uncertainties related to the design process are also
identified in structural modelling which represents the ratio between the actual and the
foreseen model's response.
According to Pugsley (1973), the main factors which may affect "proneness to structural
accidents" are [4]:
− new or unusual materials;
− new or unusual methods of construction;− new or unusual types of structure;− experience and organization of design and
construction teams;
− research and development background;− financial climate;− industrial climate;− political climate. Table 2 Prime causes of failure.
Adapted from Walker (1981)
All these factors fit very well in the field of long span structures involving oftenly something
"unusual" and clearly have an influence affecting human interaction.
In Table 2, the prime cause of failure gives 43% probability (Walker, 1981) to inadequate
appreciation of loading conditions or structural behaviour. Apart from ignorance and
negligence, it is possible to observe that the underestimation of influence and insufficient
knowledge are the most probable factors in observed failure cases (Matousek & Schneider,
1976).
Performance and serviceability limit states violation are also directly related to structural
reliability. Expertise in structural detail design, which is normally considered as a micro task
in conventional design, have an important role in special long span structures: reducing the
model and physical uncertainties and avoiding chain failures of the structural system.According to the author, knowledge and experience are the main human intervention factors
to filter gross and statistical errors in the normal processes of design, documentation,
construction and use of structures.
The reliability of the design process in the field of special structures must be checked in the
following three principal phases: the conceptual design, analysis, and working design phases.
Due to the lack of space, only some design & analysis illustrations of wide span enclosures,
where the author was directly involved, will be included in the present paper with the
intention to transmit some experiences, that today may be part of the knowledge base,
specially addressed to loading analysis and structural behaviours.
Long span structures needs special investigations concerning the actual live load distribution
and intensity on large covering surfaces. Building codes normally are addressed only to small-
Cause %
Inadequate appreciation of loadingconditions or
structural behaviour
43
Random variations in loading,structure, materials, workmanship,
etc.
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medium scale projects. The uncertainties relate to the random distribution of live loads on
long span structures imply very careful loading analysis using special experimental analysis.
From the direct author's experience in designing large coverings, the most important
experimental investigation regarding live load distribution concerns the snow drift and
accumulation factors and the dynamic action of wind loading.
2. DESIGN ASSISTED BY EXPERIMENTAL ANALYSIS
2.1. Snow loading experimental analysis on scale models
Olympic Stadium in Montreal. During the design of the new roof for the Montreal Olympic
Stadium (Figure 3) a special analysis of snow loading was made considering three roof
geometries varying the sag of the roof from 10 m, 11.5 m and 13 m, in order to find a
minimization of snow accumulation.
Snow loads depend on many cumulative factors such as, snowfall intensity, redistribution of
snow by the wind (speed and direction), geometry of the building and all surroundingsaffecting wind flow patterns, absorption of rain in the snowpack, and depletion of snow due to
melting and subsequent runoff.
The experimental investigation was carried out by RWDI [5] to provide design snow
according to FAE (Finite Area Element) method, representing up to day a state of the art on
the matter.
The shape of the roof with a sag of more than 12m. gives separation of the air flow and
turbulence in the wake increasing considerably the possibility of snow accumulations. The
order of magnitude of the leopardized accumulations in the roof are of 4-15 kN; local
overdimensioning was necessary in order to avoid progressive collapse of the structural
system.
Figure 3. Montreal Olympic Stadium.
A cable stayed roof solution
Figure 4. Comparative analysis of snow loading
distribution in function of roof shape (10-13m)
2.2. Wind loading-experimental analysis on scale models: rigid structures-quasi static
behaviour
The Cp factors: The Olympiakos Stadium in Athens
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The stadium is located near to the sea, as a consequence a “sea wind profile” with the
parameters listed below and taken from literature and laboratory expertise, seems to be a good
approximation of the wind profile in the area (Fig.6):
profile exponent α = 0.15 ÷ 0.18 (level ground, with few obstacles, sea),
roughness length z0 = 5 ÷15 cm (cultivated fields),integral length scale LU = 50÷100 m.
Figure 5. 3D rendering of the
Olympiakos
Stadium in Athens
Figure 6. Geographic location of the
stadium
10-1
100
101
102
103
10-2
10-1
100
-40 -30 -20 -10 0 10 20 30 40 50 60-40
-30
-20
-10
0
10
20
30
40
Cp
MIN (Top- Bottom) [file: dati-0000]
-2.50
-2.19
-1.88
-1.56
-1.25
-0.94
-0.63
-0.31
0.00
0.31
0.63
0.94
1.25
1.56
1.88
2.19
2.50
N
Figure 7. Spectral density of the
longitudinal component of the windvelocity (“fitting” with Von Karmán
spectral density)
Figure 8. Maximum and minimum values
of net pressure coefficients (wind direction:0°).
The model has been made in a geometric scale of 1:250 and includes: the roofing, the stands,
all the structures of the stadium, and other private and public buildings not far then 250 m (in
full scale) (fig. 5) from the centre of the stadium. The geometric scale has been chosen in
order to fulfil the similitude laws (fig. 7).
The roofing has been equipped with 252 pressure taps, of which 126 at the extrados and 126at the intrados, in order to get the net pressures on the roofing. The location of the pressure
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taps has been chosen to cover the whole roofing surface according to the fig. 8, which shows
also the influence area of each pressure tap.
The pressure measurements have been performed using piezoelectric transducers linked to the
pressure taps through Teflon pipes.
Measurement and use of load time histories: The Thessaloniki Olympic sport complex
The integration of the wind tunnel data into the design process presents significant problems
for wide span sub-horizzontal enclosures; in contrast to buildings (high rise buildings) where
knowledge of the base moment provides a sound basis for preliminary design, there is not
single simple measure for the roof. The study of the Stadium of the Alpes and the Rome
stadiums [6-7-8] drew attention to the inability of the measuring system employed to provide
data in a form that could readily be based as input to the sophisticated dynamic numerical
model developed by the designer and lead to discussion between the designer and the wind
tunnel researchers to examine alternate techniques that might be used in future projects.The
discussions centered on the use of high speed pressure scanning systems capable of producing
essentially simultaneous pressure measurements at some 500 points at rates of perhaps 200Hz per point. With such a system it would be possible to cover in excess of 200 panels and
produce a complete description of the load. Such a system would produce roughly 1 to 2x106
observations for a single wind direction and it is clear that some compression of the data
would be required. One possible approach would be to produce a set of load histories, Qj(t),
such that:
∫= A
j j dA y xt y x pt Q ),(),,()( φ (1)
where:
p(x,y,t) nett load per unit area at position (x,y);
( ) y x j ,φ weighting function.
For a series of pressure taps of the approximation to )(t jφ would be:
∑=
= N
i
ii jiiii j y x At y x pt Q1
),(),,()( φ (2)
Ai area of ith panel;
pi pneumatic average of pressure at the taps in the ith panel;
xi, yi geometric centre of the taps on the ith panel;
N number of panels.
In collaboration with the Boundary layer wind tunnel laboratory of the University of Western
Ontario, a new very practical method to obtain the structural response under the random wind
action and small displacements (linear response) has been applied under the name of the
“orthogonal decomposition method” [7-9].
The experiment would involve the recording of the local histories )(t jφ from which the model
time histories could be constructed and the analysis conduced in either the time or frequency
domain (fig. 9-10). For the type of structure under consideration resonant effects are small
and the response is largely a quasi-static to a spatially varied load. The deflections induced are
closely related to the imposed loads and their distribution differs significantly from the
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Gaussian form [6]. In such a case the time domain solution, which preserves the extreme
value distribution, is to be preferred over a frequency domain approach.
Figure 9. Views of pressure model of
Thermis Sport Hall
Figure 10. Orthogonal decomposition:
pressure mode shapes
2.3. Wind loading-experimental analysis on scale models : flexible structures-
aerodynamic behaviour: The olympic stadium in Rome
The wind induced response of the cable supported stadium roof was analysed by a non linear
model and a field of multicorrelated artificial generated wind loading time histories [7].Wind
tunnel tests have been carried out at the BLWT Lab. of UWO on a model of 1:200 (fig. 11)
scale determining:
- time histories of the local pressures for every 10° of incoming flow direction;the
maximun,minimun and average values of the wind pressure have then been evaluated, as well
as the root mean square of its fluctuating part;- presssure coefficients (maxima,minima and average) for every 10° of incoming direction;
- auto and cross-spectra of the fluctuating pressure (averaged on every single panel).
Figure 11. Aeroelastic model for
Rome Olympic Stadium
Figure 12. Aeroelastic model for the
Braga Stadium
The aerodynamic behaviour shows a clear shedding phenomenon. The external border of the
structure, constituted of the trussed compression ring with triangular section and tubular
elements and by the roofing of the upper part of the stands, disturbs the incoming horizontal
flow in such a way so that vortex shedding is built up. This causes the roofing structure to besubjected to a set of vortices with a characteristic frequency. This is confirmed by the
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resulting Power Spectra Density Function of the fluctuating pressures, which shows a peak at
about 0.15Hz even if the values rapidly decrease with increasing distance (fig. 13).
Figure 13. Target (1), simulated (2)
and Kaimal's (3) normalized spectra
of wind velocity
Figure 14. Time History of the
displacement (leeward side at tension
ring, run #2)
A fluid-interaction non linear analysis in time domain, made for the checking of La Plata
stadium design [10] shows a better agreement between theoretical model and experimental
values.
3. RELIABILITY ANALYSIS: THE SENSIBILITY ANALYSIS REGARDING THE
NEW SUSPENDED CABLE ROOF OF BRAGA (PORTUGAL)
3.1. Reliability analysis of the roof structural system. Cable strain parametric sensibility.
Considering that in the basic solution the roof will be covered by a long span structural
system with only uplift gravitational stabilization (fig. 17) it is essential to proceed to theanalysis of the response of the structural system to loading patterns and wind induced
oscillations.
The analytical process will be organized in order to be controlled by experimental
investigations in reduced and full scale.
The reduced scale experimental analysis on rigid and aeroelastic models are concerned with
the determination of the dynamic loading on the roof surface and of the stability of the
structural system.
The full scale experimental investigations are addressed to check, by a monitoring program,
the validity of the global analysis process.
The uncertainties on the elastic modulus of the cable, geometrical and elastic long term
creeping, tolerances of fabrication and erection, differences with design prestress, non
uniform distribution of temperature, non linear behaviour, created a sensitive response on the
suspended roof hanging from a set of suspended cables. The sensibility analysis showed that
the response is sensitive to the standard deviation of the cable strain (∆ε) variations. Thefailure probability is given by the probability that an outcome of the random variables (∆ε)belongs to the failure domain D. This probability is expressed by the following integral [11]:
( )∫ ∆⋅∆= ∆ f D
f d f P ε ε ε (3)
and the most probable failure mechanism will involve primarily the border cables.
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x y, Beta 0〈 〉
,( )
The sensibility analysis was, therefore, extremely important to detect the weak points of the
structural system and permits proper local dimensioning to prevent chain failure, as illustrated
with the failure simulation of same sensitive cable elements.
The roof is composed by a structural concrete plate sustained by n prestress cables. In the
analysis the roof, the bending moments at m points will be considered. For a particular load
combination, the n cables have computed strains given by the vector ε. Considering that theseeffects are represented by the vector of random variables ∆ε with mean values µ and standardvariations σ, the problem is to estimate the probability, Pf, that the generated random bendingmoments M will be larger than the plate ultimate resistance moments, Mu, at any of the m
points of the structural plates system.
Figure 15.The new suspended cable roof of
Braga Stadium
(Portugal)
Figure 16. β-Safety Index
distribution, evidencing SLU
sensibility on black region
(β=3.798)
3.2. Results and conclusions
All the load cases were analysed and the following preliminary
conclusions are described as follows.
In order to identify the most dangerous load case the minimum
reliability index β for each load cases were calculated for astandard deviation σ =0.5 x 10-3 for ∆ε of all cables. Thefollowing table (Table 3) summarizes the index β (computedwith σ =0.5 x 10-3).
The load cases 7, 9 and 10 have the lowers β, i.e., the higherfailure probability, and therefore they are the critical load
condition. Particularly critical is the load case 7.
3.3. Failure probability and sensibility analysis
The figure 17 shows the failure probability for load
combination 7 as a function of the standard deviation, σ, of the
cable strain variations, ∆ε.
Load Case Beta Phi(-Beta)
1 5.8739 2.14E-09 2 5.7957 3.42E-09 3 5.9555 1.31E-09 4 5.5733 1.26E-08 5 4.1218 1.87E-05 6 4.8436 6.41E-07 7 1.6658 4.79E-02
8 5.7281 5.11E-09 9 5.5396 1.53E-08 10 2.6269 4.31E-03 11 2.3812 8.63E-03 12 4.3046 8.37E-06 13 4.3045 8.37E-06 14 5.8201 2.96E-09 15 5.7479 4.55E-09 16 5.8415 2.61E-09
Table 3. Reliability index β
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a. The problem is extremely sensitive to the standard deviation, σ, of the cable strainvariations, ∆ε. For example for load case 7, if σ is increased from 2x10-4 to 3x10-4, Pf is
increased from 2x10-5 to 480x10-5.
b. Cable standard deviation, σ, should be maintained below 2x10-4 for the designedultimate bending moment.
c. Larger cable standard deviation, σ, could be allowed increased the slab reinforcementalong x-direction in the critical roof zone.
The figure 16 shows the most probable values of ∆ε (x10-3) in each cable at failure for load
combination 7.
1.00E-08
1.00E-07
1.00E-06
1.00E-05
1.00E-04
1.00E-03
1.00E-02
1.00E-01
1.00E+00
0.00E+00 1.00E-04 2.00E-04 3.00E-04 4.00E-04 5.00E-04 6.00E-04 7.00E-04
Cable Deformation Standard Deviation
F a i l u r e P r o b a b i l i t y
-0.30000 -0.20000 -0.10000 0.00000 0.10000 0.20000 0.30000 0.4000
1
3
5
7
9
11
13
15
17
19
21
23
25
27
29
31
33
Figure 17. Failure probability in
function of cable deformation
standard deviation
Figure 18. Most probable ∆ε ineach cable at failure for load
comb. 7
4. CONCLUSIONS
It has been noted the influence of knowledge base on conceptual design in removing gross
human intervention errors from initial design statements.
Design assisted by experimental investigation is a useful integration of the design process of
wide span structures.
Sensibility analysis is an extremely powerful tool to determine the influence of parametric
design uncertainties for unusual long span structural systems.
In the last full pages figures some designs and realizations, where the writer was involved as
structural designer ,are illustrated.
5. REFERENCES
[1] H. Engel, Tragsysteme, Deutsche Verlags-Anstalt, 1967.
[2] M. Majowiecki: Observations on theoretical and experimental investigations on
lightweight wide span coverings, International Association for Wind Engineering, ANIV,
1990.
[3] Structural Design Of Retractable Roof Structures, IASS working group n°16, WIT Press,
2000
[4] R.E. Melchers: Structural reliability, Elley Horwood ltd. 1987.
[5] RWDI: Roof snow loading study-roof re-design Olympic Stadium Montreal, Quebec.Report 93-187F-15, 1993.
[6] B.J. Vickery, M. Majowiecki: Wind induced response of a cable supported stadium roof.Journal of Wind Engineering and Industrial Aerodynamics, 1992, pp. 1447-1458,
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[7] B.J. Vickery: Wind loads on the Olympic Stadium - orthogonal decomposition and
dynamic (resonant) effects. BLWT-SS28A, 1993.
[8] M. Majowiecki: Snow and wind experimental analysis in the design of long span sub-
horizontal structures, J. Wind Eng. Ind. Aerodynamics, 1998.
[9] M. Majowiecki, F. Zoulas, J. Ermopoulos: “The new sport centre in Thermi
Thessaloniki”: conceptual design of the structural steel system, IASS Congress Madrid,
september 1999.
[10] M. Lazzari, M. Majowiecki, A. Saetta, R. Vitaliani : “Analisi dinamica non lineare di
sistemi strutturali leggeri sub-horizzontali soggetti all’azione del vento”,5° Convegno
Nazionale di Ingegneria del vento, ANIV; Perugia 1998.
[11] A.G. Puppo, R.D. Bertero, : “Evaluation of Probabilities using Orientated
Simulation”, Journal of Structural Engineering, ASCE, Vol. 118, No. 6, June 1992.